Analytical investigation of an inflatable landing system having omnidirectional and multiple impact capabilities
Inflatable landing system investigated for impact normal to smooth surface
Dexter, C. B.↗
Engineering topics
Publications and source records attributed to Hathaway, M. E..
Inflatable landing system investigated for impact normal to smooth surface
Effect of heat shield flexibility on water landing loads of Apollo spacecraft models
Energy dissipating shock absorbing system for land payload recovery or vehicle braking